CH385077A - Impennaggio ad alette retrattili - Google Patents

Impennaggio ad alette retrattili

Info

Publication number
CH385077A
CH385077A CH1092061A CH1092061A CH385077A CH 385077 A CH385077 A CH 385077A CH 1092061 A CH1092061 A CH 1092061A CH 1092061 A CH1092061 A CH 1092061A CH 385077 A CH385077 A CH 385077A
Authority
CH
Switzerland
Prior art keywords
fletching
retractable fins
retractable
fins
Prior art date
Application number
CH1092061A
Other languages
English (en)
Italian (it)
Inventor
Moratti Francesco
Tosti Carlo
Original Assignee
Bombrini Parodi Delfino Spa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bombrini Parodi Delfino Spa filed Critical Bombrini Parodi Delfino Spa
Publication of CH385077A publication Critical patent/CH385077A/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
CH1092061A 1960-10-12 1961-09-20 Impennaggio ad alette retrattili CH385077A (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1757960 1960-10-12

Publications (1)

Publication Number Publication Date
CH385077A true CH385077A (it) 1965-02-26

Family

ID=11150442

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1092061A CH385077A (it) 1960-10-12 1961-09-20 Impennaggio ad alette retrattili

Country Status (5)

Country Link
US (1) US3127838A (fr)
BE (1) BE608385A (fr)
CH (1) CH385077A (fr)
DE (1) DE1168804B (fr)
GB (1) GB966035A (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
US3304030A (en) * 1965-09-24 1967-02-14 James E Weimholt Pyrotechnic-actuated folding fin assembly
SE340417B (fr) * 1969-06-06 1971-11-15 Bofors Ab
NL7017521A (fr) * 1969-12-03 1971-06-07
DE2841773C2 (de) * 1978-09-26 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Anordnung des Leitwerks, insbesondere bei Flugkörpern oder Geschossen
US4480806A (en) * 1982-11-08 1984-11-06 Stencel Aero Engineering Corporation Ejection seat stabilization apparatus
US4664339A (en) * 1984-10-11 1987-05-12 The Boeing Company Missile appendage deployment mechanism
US4667899A (en) * 1984-11-28 1987-05-26 General Dynamics, Pomona Division Double swing wing self-erecting missile wing structure
DE3508103A1 (de) * 1985-03-07 1986-09-18 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Falt-/klappfluegel
FR2623898B1 (fr) * 1987-11-26 1990-03-23 France Etat Armement Dispositif de deploiement d'une ailette de projectile
US4869442A (en) * 1988-09-02 1989-09-26 Aerojet-General Corporation Self-deploying airfoil
FR2655720A1 (fr) * 1989-12-08 1991-06-14 Thomson Brandt Armements Aile galbee deployable pour engin volant.
US6928400B2 (en) * 2001-10-02 2005-08-09 Raytheon Company Method for designing a deployment mechanism
AU2002346422A1 (en) * 2002-11-18 2004-06-15 Raytheon Company Method for designing a fin deployment mechanism
US7642492B2 (en) * 2005-01-26 2010-01-05 Raytheon Company Single-axis fin deployment system
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
US10458764B2 (en) 2016-10-24 2019-10-29 Rosemount Aerospace Inc. Canard stowage lock
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
US11754379B2 (en) * 2018-03-23 2023-09-12 Simmonds Precision Products, Inc. Space saving wing stowage
CN110360897A (zh) * 2019-06-28 2019-10-22 南京理工大学 一种稳定的超空泡射弹入水结构
US11187505B1 (en) * 2019-07-03 2021-11-30 Gerhard W. Thielman Concatenated annular swing-wing tandem lift enhancer

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1048514B (fr)
GB189523823A (en) * 1895-12-12 1896-11-14 Martns Stevenson Calvert Improvements in Projectiles.
BE379532A (fr) * 1930-05-22
US2700337A (en) * 1952-02-28 1955-01-25 James M Cumming Liquid propellent rocket
FR1187193A (fr) * 1957-11-15 1959-09-08 Hotchkiss Brandt Empennage déployant perfectionné pour projectile
FR1191519A (fr) * 1958-02-13 1959-10-20 Hotchkiss Brandt Empennage déployant pour projectile d'artillerie
US3063375A (en) * 1960-05-19 1962-11-13 Wilbur W Hawley Folding fin

Also Published As

Publication number Publication date
DE1168804B (de) 1964-04-23
US3127838A (en) 1964-04-07
BE608385A (fr) 1962-01-15
GB966035A (en) 1964-08-06

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